FR2913747B1 - Procede de realisation de raidisseurs en materiau composite - Google Patents

Procede de realisation de raidisseurs en materiau composite

Info

Publication number
FR2913747B1
FR2913747B1 FR0701947A FR0701947A FR2913747B1 FR 2913747 B1 FR2913747 B1 FR 2913747B1 FR 0701947 A FR0701947 A FR 0701947A FR 0701947 A FR0701947 A FR 0701947A FR 2913747 B1 FR2913747 B1 FR 2913747B1
Authority
FR
France
Prior art keywords
lateral projections
composite material
flanks
stiffeners
producing
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
FR0701947A
Other languages
English (en)
French (fr)
Other versions
FR2913747A1 (fr
Inventor
Patrick Dunleavy
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Landing Systems SAS
Original Assignee
Messier Dowty SA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority to FR0701947A priority Critical patent/FR2913747B1/fr
Application filed by Messier Dowty SA filed Critical Messier Dowty SA
Priority to JP2009553178A priority patent/JP5102316B2/ja
Priority to US12/531,565 priority patent/US8205567B2/en
Priority to BRPI0808955-8A priority patent/BRPI0808955A2/pt
Priority to CN200880008263XA priority patent/CN101631668B/zh
Priority to ES08775635T priority patent/ES2350386T3/es
Priority to CA2680923A priority patent/CA2680923C/fr
Priority to RU2009138245/05A priority patent/RU2421336C1/ru
Priority to DE602008002228T priority patent/DE602008002228D1/de
Priority to PCT/FR2008/000300 priority patent/WO2008132319A1/fr
Priority to EP08775635A priority patent/EP2121295B1/fr
Priority to AT08775635T priority patent/ATE477920T1/de
Publication of FR2913747A1 publication Critical patent/FR2913747A1/fr
Application granted granted Critical
Publication of FR2913747B1 publication Critical patent/FR2913747B1/fr
Priority to IL200803A priority patent/IL200803A0/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/543—Fixing the position or configuration of fibrous reinforcements before or during moulding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/545—Perforating, cutting or machining during or after moulding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00—Subject matter not provided for in other groups of this subclass
    • B29D99/001—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings
    • B29D99/0014—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with ridges or ribs, e.g. joined ribs
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
    • B29C53/02—Bending or folding
    • B29C53/04—Bending or folding of plates or sheets
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3076—Aircrafts
    • B29L2031/3082—Fuselages
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24033—Structurally defined web or sheet [e.g., overall dimension, etc.] including stitching and discrete fastener[s], coating or bond

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Structural Engineering (AREA)
  • Civil Engineering (AREA)
  • Architecture (AREA)
  • Textile Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Footwear And Its Accessory, Manufacturing Method And Apparatuses (AREA)
  • Manufacture Of Motors, Generators (AREA)
  • Reinforced Plastic Materials (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Shaping Of Tube Ends By Bending Or Straightening (AREA)
FR0701947A 2007-03-16 2007-03-16 Procede de realisation de raidisseurs en materiau composite Expired - Fee Related FR2913747B1 (fr)

Priority Applications (13)

Application Number Priority Date Filing Date Title
FR0701947A FR2913747B1 (fr) 2007-03-16 2007-03-16 Procede de realisation de raidisseurs en materiau composite
EP08775635A EP2121295B1 (fr) 2007-03-16 2008-03-07 Procede de realisation de raidisseurs en materiau composite
BRPI0808955-8A BRPI0808955A2 (pt) 2007-03-16 2008-03-07 Processos de obtenção de pelo menos um elemento de enrijecimento e de um painel enrijecido
CN200880008263XA CN101631668B (zh) 2007-03-16 2008-03-07 制作复合材料的加强材的方法
ES08775635T ES2350386T3 (es) 2007-03-16 2008-03-07 Procedimiento de realización de elementos de refuerzo de material compuesto.
CA2680923A CA2680923C (fr) 2007-03-16 2008-03-07 Procede de realisation de raidisseurs en materiau composite
JP2009553178A JP5102316B2 (ja) 2007-03-16 2008-03-07 複合材料の補剛材を製造する方法
DE602008002228T DE602008002228D1 (de) 2007-03-16 2008-03-07 Verfahren zur herstellung von versteifungen aus einem verbundwerkstoff
PCT/FR2008/000300 WO2008132319A1 (fr) 2007-03-16 2008-03-07 Procede de realisation de raidisseurs en materiau composite
US12/531,565 US8205567B2 (en) 2007-03-16 2008-03-07 Method of making composite material stiffeners
AT08775635T ATE477920T1 (de) 2007-03-16 2008-03-07 Verfahren zur herstellung von versteifungen aus einem verbundwerkstoff
RU2009138245/05A RU2421336C1 (ru) 2007-03-16 2008-03-07 Способ изготовления элементов жесткости из композиционного материала
IL200803A IL200803A0 (en) 2007-03-16 2009-09-08 A method of making composite material stiffeners

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0701947A FR2913747B1 (fr) 2007-03-16 2007-03-16 Procede de realisation de raidisseurs en materiau composite

Publications (2)

Publication Number Publication Date
FR2913747A1 FR2913747A1 (fr) 2008-09-19
FR2913747B1 true FR2913747B1 (fr) 2009-04-24

Family

ID=38669098

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0701947A Expired - Fee Related FR2913747B1 (fr) 2007-03-16 2007-03-16 Procede de realisation de raidisseurs en materiau composite

Country Status (13)

Country Link
US (1) US8205567B2 (zh)
EP (1) EP2121295B1 (zh)
JP (1) JP5102316B2 (zh)
CN (1) CN101631668B (zh)
AT (1) ATE477920T1 (zh)
BR (1) BRPI0808955A2 (zh)
CA (1) CA2680923C (zh)
DE (1) DE602008002228D1 (zh)
ES (1) ES2350386T3 (zh)
FR (1) FR2913747B1 (zh)
IL (1) IL200803A0 (zh)
RU (1) RU2421336C1 (zh)
WO (1) WO2008132319A1 (zh)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8720825B2 (en) * 2005-03-31 2014-05-13 The Boeing Company Composite stiffeners for aerospace vehicles
ES2371951B1 (es) * 2009-03-25 2012-11-21 Airbus Operations, S.L. Disposición de junta de elementos estructurales de un material compuesto.
FR2971194A1 (fr) * 2011-02-04 2012-08-10 Latecoere Procede de realisation d'une preforme elementaire formee d'un empilage de couches de renfort a structure fibreuse
FR2971193B1 (fr) * 2011-02-04 2013-04-26 Latecoere Procede de realisation d'une preforme a structure fibreuse presentant la forme d'un profile comportant une ame, et preforme realisee
FR2972387B1 (fr) * 2011-03-09 2013-04-26 Latecoere Procede de realisation d'une preforme comportant au moins deux troncons presentant des epaisseurs differentes.
GB201115080D0 (en) * 2011-09-01 2011-10-19 Airbus Operations Ltd An aircraft structure
CN103407171B (zh) * 2013-07-30 2015-07-15 北京航空航天大学 一种缝纫增强的纤维增强树脂基复合材料十字型接头的整体成型方法
EP3040191B1 (en) 2014-12-30 2019-08-07 Airbus Operations, S.L. Method for manufacturing fillers of composite material
US10434956B2 (en) * 2016-03-24 2019-10-08 Honda Motor Co., Ltd. Fabric processing method and component
US10220935B2 (en) * 2016-09-13 2019-03-05 The Boeing Company Open-channel stiffener
CN108953978A (zh) * 2018-06-19 2018-12-07 哈尔滨工程大学 一种h型腹杆和方形弦杆装配的复合材料桁架及其制备方法
JP2020142478A (ja) * 2019-03-08 2020-09-10 トヨタ自動車株式会社 成形方法
DE102019203906A1 (de) * 2019-03-21 2020-09-24 Brose Fahrzeugteile Se & Co. Kommanditgesellschaft, Bamberg Trägerbauteil mit Befestigungsbereich aus einem Faserverbundwerkstoff und mindestens einem ein Befestigungselement arretierenden Stützelement
CN112173062A (zh) * 2020-09-25 2021-01-05 中国直升机设计研究所 一种复合材料一体化框梁及制造方法

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3996084A (en) * 1974-06-17 1976-12-07 Mcdonnell Douglas Corporation Lock core panel
US4331495A (en) * 1978-01-19 1982-05-25 Rockwell International Corporation Method of fabricating a reinforced composite structure
FR2497726A1 (fr) * 1981-01-12 1982-07-16 Brochier Fils J Article textile multicouches pour le renforcement de materiaux stratifies et procede pour son obtention
FR2497839A1 (fr) * 1981-01-12 1982-07-16 Brochier Fils J Tissu tridimensionnel pour le renforcement de materiaux stratifies et elements en forme obtenus a partir d'un tel tissu
JPS5887042A (ja) * 1981-11-19 1983-05-24 東レ株式会社 繊維強化樹脂用補強材
US4622254A (en) * 1981-08-31 1986-11-11 Toray Industries, Inc. Fiber material for reinforcing plastics
JPS58117160A (ja) * 1981-12-28 1983-07-12 東レ株式会社 桁材
US4966802A (en) * 1985-05-10 1990-10-30 The Boeing Company Composites made of fiber reinforced resin elements joined by adhesive
JPH03119138A (ja) * 1989-09-29 1991-05-21 Shikishima Kanbasu Kk 繊維補強複合材
FR2687173B1 (fr) * 1992-02-11 1995-09-08 Aerospatiale Procede pour la realisation d'une armature de fibres pour piece de matiere composite, et piece composite comportant une telle armature.
FR2687389B1 (fr) * 1992-02-17 1994-05-06 Aerospatiale Ste Nationale Indle Dispositif et procede pour realiser une piece de structure complexe par depose au contact de fil ou ruban.
EP1023986B2 (en) * 1999-01-28 2012-01-18 McDONNELL DOUGLAS CORPORATION Reinforcing member of composite workpieces and associated methods
GB2370587B (en) * 2000-12-12 2002-11-13 Intelikraft Ltd Reinforced material
US6896841B2 (en) * 2003-03-20 2005-05-24 The Boeing Company Molding process and apparatus for producing unified composite structures

Also Published As

Publication number Publication date
FR2913747A1 (fr) 2008-09-19
US8205567B2 (en) 2012-06-26
BRPI0808955A2 (pt) 2014-08-26
WO2008132319A1 (fr) 2008-11-06
ES2350386T3 (es) 2011-01-21
CN101631668A (zh) 2010-01-20
CA2680923C (fr) 2011-08-02
EP2121295B1 (fr) 2010-08-18
JP5102316B2 (ja) 2012-12-19
ATE477920T1 (de) 2010-09-15
RU2421336C1 (ru) 2011-06-20
CA2680923A1 (fr) 2008-11-06
IL200803A0 (en) 2010-05-17
RU2009138245A (ru) 2011-04-27
CN101631668B (zh) 2013-02-27
US20100096067A1 (en) 2010-04-22
EP2121295A1 (fr) 2009-11-25
JP2010521336A (ja) 2010-06-24
DE602008002228D1 (de) 2010-09-30

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Legal Events

Date Code Title Description
TP Transmission of property

Owner name: MESSIER-BUGATTI-DOWTY, FR

Effective date: 20110922

ST Notification of lapse

Effective date: 20131129